[0001] The present invention relates to a laser device method to arrange and adjust a laser
device, with a single adjustment parameter to set device in a lasing condition to
emit at a wavelength, where deviation between a predetermined wavelength and the sole
wavelength, at which the device is capable of lasing is being dependent on the mechanical
precision with which the device can be manufactured and lined up, which laser device
comprise optical components including laser element, which can generate optical radiation
within a wavelength band, optical collimator, which inside the laser collimates radiation
emitted from the laser element, and plane reflection grating with parallel grating
grooves, arranged such that the latter together with a flat reflection surface, which
can be one end surface of the laser element, forms a resonator, which selects the
radiation wavelength emitted by the laser device.
Background of the invention
[0002] Small, simple and stable lasers with a long term of life, that are spectrally pure
and have a well defined optical frequency, are lacking today. Solid state lasers,
e.g. in the shape of semiconductor elements that are equipped with an external cavity,
would fulfil the requirements if they can be made small and stable. Such a laser can
from a practical point of view be termed a
fixed frequency laser.
[0003] A simple stable laser, with essentially corresponding practical properties as the
fixed frequency laser, but having a wavelength that stays fixed in the environment
of usage is also a desired object. Such a laser, which adapts its frequency in a fashion
that the radiation wavelength remains constant, even when the atmospheric environment
or some other surrounding gaseous environment varies, e.g. with respect to pressure
and temperature, may be termed a
fixed wavelength laser.
[0004] It may be of practical interest to let the term
fixed laser comprise the two variants, the fixed frequency laser and the fixed wavelength laser.
The prefix fixed implies that the frequency or wavelength from a practical point of
view remains constant with respect to unintentional influences from the inner and
outer environment, e.g. change in temperature, mechanical shock or change in humidity.
The prefix has on the other hand no bearing on the possibility of controlling the
frequency. Intentional alternation or modulation of the frequency is presupposed in
various embodiments of the fixed laser, e.g. through geometrical alternation of the
cavity of the laser device by forces from piezoelectric elements, through change of
the temperature of the laser element etc.
[0005] In many applications it may suffice that the laser has a fixed frequency, but it
may not be necessary that the frequency has a given value or that it can be altered.
This may be the case, e g when the laser is used as an optical source for interferometric
measurements in a stable outer environment, or when the requirements on measurement
accuracy are moderate. Typical applications are measurements of geometrical dimensions
or recordings of the change in position of an object, e.g. in manufacturing industry.
[0006] Another class of applications in which it may suffice that the fixed laser has a
fixed frequency, that does not need to be altered, comprises usages of the laser as
a local oscillator in measurements of the variations of the optical frequency of a
laser light source.
[0007] Shall the laser on the other hand be used for accurate interferometric measurements
in an outer environment with varying air parameters then it is necessary to keep the
air wavelength of the laser radiation constant, which implies that the frequency shall
be adjusted along with the variations in the air parameters.
[0008] In many intended applications of the fixed laser it is necessary to be able to control
its frequency. In spectroscopic applications of the fixed laser, e.g. in analysis
of gases, one must be able to adjust its frequency to coincide with the frequency
of an absorption line. Alteratively one must be able to sweep the frequency across
a region that includes the absorption line.
[0009] Another field in which one must be able to control or modulate the frequency of the
fixed laser, e g through changing the external cavity by piezoelectric or similar
forces, is optical communication and other applications which imply transmission of
information.
[0010] To sum up, the fixed laser can be expected to find many applications as an optical
source of radiation in applications concerned with measurements, analysis, sensing
and information technology.
[0011] A realization of the fixed laser requires new solutions to a number of technical
problems.
[0012] In conventional mechanical manufacturing and alignment of optical components in a
laser device only a limited precision can be achieved. In terms of position and angular
attitude this may typically be 10µm and 1 milliradian respectively. By using more
costly manufacturing methods the precision can be increased somewhat. The tolerances
mentioned are not sufficient to keep the external cavity adjusted for lasing, i.e.
in a state that it can emit laser radiation. To achieve this, adjustments are required
to an accuracy of a tenth or a few tenths of a µm in position and a tenth or few tenths
of a milliradian in angle.
[0013] European patent application no. 335.691, shows an external cavity laser assembly
in which the laser chip is within a hermetically sealed package and the external cavity
is outside the hermetic package. A collimator lens in a screw threaded mounting is
disposed outside the hermetic package, the screw threaded permitting focusing. The
cavity is tuned by rotation and translation of the a grating, the position of which
is electrically controlled via piezoelectric stacks. In the laser device according
to the above application only the chip is packaged within a hermetic package; the
laser is only toned through rotation and translation of the grating using piezoelectric
stacks; thermal expansion of the stacks is compensated using proper housing material;
and the refractive index variations, due to the temperature variations are not compensated.
The object of the invention and its most important characteristics
[0014] A first object of the invention in question is to achieve a fixed laser with small
dimensions and a long term of life, that is spectrally pure and has a well defined
optical frequency and a minimal dependence on changes in the inner and outer environment,
e.g. on alterations in temperature and pressure.
[0015] A second object of the invention in question is to achieve a fixed laser of a simple
construction, that is easy to assemble, and that only requires a minimal effort to
adjust, and that is possible to fix in the adjusted position such that it retains
its frequency.
[0016] A third object is to achieve a fixed laser in which the frequency can be controlled
or modulated, e.g. by a geometrical alteration of the external cavity.
[0017] A fourth object is to achieve a fixed laser in which the wavelength of the radiation
remains constant in a varying outer air or gas environment.
[0018] The above objects of the invention are attained through the means specified in the
accompanying patent claims.
[0019] A basic observation in the invention is that there are two directions essential to
the procedure of lining up a laser device that has a grating resonator, the direction
L O of the collimated radiation and the direction G of the grating grooves. When these
two directions become perpendicular, the laser device has been lined up and radiation
having a wavelength, which is determined by the grating equation.

is returned from the grating in a direction opposite to that of the incident radiation.
In (1) λ is the radiation wavelength, N
o the grating order, d the distance between consecutive grating grooves and α the angle
of incidence of the radiation with respect to the grating. The returning radiation
is focused by the lens device, that has collimated the radiation, to the point or
spot of the laser element from which the radiation has been emitted. Thus if the angle
Φ between the two directions mentioned above is 90° the device has been aligned for
lasing. There is, however, still another prerequisite for lasing to occur.
[0020] The laser element must be able to emit radiation at the wavelength λ
o, which satisfies the grating equation (1). The exact value α
o of α has not been predetermined, but deviates in the fabrication of the device, and
in procedure of adjusting Φ, somewhat from an assumed or nominal value. The laser
element must thus be able to emit radiation within a wavelength range which contains
λ
o.
[0021] In using a semiconductor laser element, which is one type of laser elements intended
for the fixed laser, it is not difficult to fulfil the requirement that λ
o shall fall within the radiation range of the laser element. A semiconductor laser
element, nominally radiating at λ = 1.55 µm, can typically be used for generating
laser radiation within a range 1.50 - 1.60 µm. According to the grating equation,
using No = 1, λ
o = 1.55 µm and α
o = 45°, the range λ
1-λ
2 = 1.55 ± 0.05 corresponds to an angular range α
1 - α
2 = 45°± 2°. The angle α can thus be easily preset such that λ falls in the wavelength
range for potential lasing.
[0022] The direction of the collimated radiation is defined by the line LO in fig 1, that
runs between the aperture of the laser element, which in case of a semiconductor element
is the end surface of a radiation channel about 1 µm wide, and the optical center
O of the lens. The tilt of the lens with respect to the line in question is not very
critical. This corresponds to the fact that one gets a good point image in the focal
plane with parallel near axial rays.
[0023] The requirement discussed earlier to have an accuracy of a tenth or a few tenths
of a µm in the adjustment of the position of an optical component refers to a plane
that contains the direction of collimation LO and the direction G of the grating grooves
and concerns changes in the direction G. The corresponding requirement on the accuracy
in the angular adjustment refers to the angle in the plane just mentioned.
[0024] The adjustment in the direction of collimation, e.g. of the distance between the
lens and the laser element, has to be made with an accuracy, that is perhaps ten times
lower than the accuracy required for changes in the direction G. A possible way is
to separately manufacture and adjust a unit consisting of a lens and a laser element.
A small trimming of the cavity length with up to λ/4, that may be needed to avoid
that the laser oscillates in an unstable position between two modes, can best be done
with the laser running through a change of the refractive index of the laser element,
e.g. via the electric current through the element or via the temperature of the element.
[0025] A background assumption to the invention is that it should be possible to manufacture
and assemble the structural components of the fixed laser, holders for optical components
and the like, using conventional workshop precision. A basic idea in the invention
is that after the assembly of the fixed laser, the final adjustment of it to optimal
lasing, at a not entirely predetermined wavelength λ
o within the band λ
1 - λ
2, can be made by rotation of one of the optical components of the laser, which is
then fixed.
[0026] Fig. 2 and 3 show examples of possible final rotational adjustments. If for instance
the laser element 1 is rotated about a fixed axis K that is approximately perpendicular
to the direction G of the grooves, then the line LO, that is the line between the
aperture L of the laser element and the optical center O of the lens, oscillates and
describes a cone that has its tip in O. If instead the lens is rotated in a similar
fashion, then the line LO at some angle of rotation becomes perpendicular to the grating
grooves, that is Φ = 90°. The choice of cone angle determines how large a portion
of a complete revolution one has to turn in order to be sure to reach the state Φ
= 90°.
[0027] The rotation of one component, e.g. the laser element, can for instance be done by
having it placed eccentrically in a cylindrical tube whose axis becomes the axis of
rotation K. If the lens is symmetrically placed in the tube that turns the laser element,
then the conical pendulous movement of L0 becomes the same as with the lens spatially
fixed.
[0028] When it is the laser element that is turned one has reason to choose the conical
angle sufficiently large that the element does not get a change in attitude, that
would be troublesome with respect to the polarization of the radiation. The corresponding
problem arises if one instead turns the grating. It does not, however, occur when
it is the lens that is turned.
Description of the drawings
[0029] The invention will be further described below with reference to the attached drawings,
which show examples of embodiments of the invention.
[0030] Fig. 1 shows schematically the positions of the optical components of the laser according
to the present invention.
[0031] Fig. 2 shows turning of the laser element in order to alter the direction of collimation
LO in the laser according to the present invention
[0032] Fig. 3 shows turning of the lens on order to alter the direction of collimation LO
in the laser according to the present invention
[0033] Fig. 4 shows a central section along the main axis A in a first embodiment of a fixed
laser according to the present invention
[0034] Fig. 5 shows a central section of the fixed laser in Fig. 4 with its plane perpendicular
to that of the section of Fig. 4
[0035] Fig. 6 shows a central section along the main axis A in a second embodiment of a
fixed laser according to the present invention
[0036] Fig. 7 shows a frontal view of an example of a laser element holder with an arrangement
for adjustments in a fixed laser according to the present invention
[0037] Fig. 8 shows welding seams in a fixed laser according to the first embodiment of
the present invention
[0038] Fig. 9 shows a fixed laser according to the present invention provided with active
temperature control and thermal insulation
[0039] Fig. 10 shows a fixed laser arrangement for keeping the radiation wavelength constant
in an outer environment according to the present invention, which is controlled by
feeding back a signal from a wavelength sensing interferometer that is firmly attached
to the laser and is in atmospheric contact with the outer environment.
[0040] Fig. 11 shows the arrangement of Fig. 10 to which has been added a further laser,
optical components which bring the emission from the two lasers together, and a photodetector
of the two laser emissions as a measure of changes in the refractive index of the
outer environment according to the present invention.
[0041] Fig. 12 shows sections of fixture devices for common application of holographic grating
on a number of seat taps. a) Device for holographic layer application directly on
the seat taps b) Device for holographic layer on a base which is fixed to the seat
taps.
[0042] Fig. 13 shows a laser attachment of hinge type with soldering tongue.
a) Front view of the attachment
b) section A-A perpendicular to the plane in a)
[0043] Fig. 14. Joining of base plate, insulator block and soldering tongue at simultaneous
manufacture of many laser attachments
a) Part of continuous sheet of base plates and details from soldering tongue sheet
and block assembly
b) Section B-B perpendicular the front view in a)
Description of embodiments
[0044] The fixed laser has in a first embodiment see Fig. 4, a main body 10, that is rotationally
symmetric, and has a central axial lining-up bore 17 with a main axis A. A grating
seat 13, which has a tap 7 with a cylindrical fit, that may be very high, ± 0,5 µm,
is inserted into the lining-up bore. The lens 2 is fixed in the tube 12, which in
turn is inserted into the tube 11. The optimal position of 12 relative to 11 is tested
separately, for instance in an adjustment fixture and it is checked that the radiation
5 is collimated at a predetermined nominal wavelength. After that 11 and 12 are fixed
relative to each other, for instance by welding.
[0045] The laser element 1 and the collimator lens 14, used for collimating the beam 15
leaving the laser, are mounted on the tubes 11 and 6 respectively, which are fitted
to two turned holds on the main body 10. The components are thus put together according
to a telescopic principle, with the axes of all tubes coinciding with the main axis
A. A deviation from the rotational geometry is that the grating 3 is mounted on an
obliquely chamfered tap of the seat 7, and means on the tube 11 for fixing the laser
element 1. In order to adjust the position of the laser element the tube 11 can be
turned about the main axis A until the radiation from the fixed laser shows, that
the angle Φ has been turned to 90°. After that the tube 11 is fixed to the main body
10.
[0046] In the example given of a first embodiment of the fixed laser, the laser element
1 is eccentrically placed on the tube 11 such that its deviation from the symmetry
axis A is 10-50µm. During the mounting of the element 1 its position is checked in
a microscope or through inserting into the tube 11 a gauge with cylindrical fit and
which has position markings. A central symmetrical positioning of lens 2 in the tube
12 can easily be done with sufficient precision without the use of special measuring
gauges.
[0047] The example of a first embodiment of the fixed laser can be varied as to a number
of design details. The carrier tubes for the optical components can thus be mounted
on the main body 10 in other ways than has been shown in the example. The tubes 11
and 12 can for instance be inserted into, or slipped on to the main body in other
ways, than has been exemplified. It is for example also possible to let one or several
of the component carrying tubes have another axis of rotation K than the main axis
A.
[0048] Fig. 6 shows an example in variation of mounting. It is a second embodiment of the
grating mounting in a fixed laser, in which the rotational symmetry of the main body
10 about the main axis A has been abandoned. The advantage of this arrangement is
that the grating is mounted perpendicularly to the cylindrical tap 7 of the seat,
which is inserted in an oblique bore in the main body 18, in such a way that the normal
to the grating surface will form a predetermined angle α to the collimated radiation
in the laser. Also the fixing of the adjusted optical components can be made in a
number of other ways than by welding, e g by soldering or cementing.
[0049] As is evident from the above the fixed laser according to the present inventions
is based on a rotational symmetry in most of the components. It can be given an extremely
compact structure, which the laser device having dimensions of about 10 x 20 mm. It
is easy to mount, Fig. 8, and to line up. The rotationally symmetric details are potentially
cheap to produce. They also give the advantage that shortcomings due to thermal expansions
crosswise are avoided.
[0050] Fig. 9 shows one embodiment of thermal stabilization of the laser device. A thermally
insulating material 38, e.g. silicone rubber, polyurethane or polystyrene is applied
between a cooling flange 40 and an inner tube 39, which serves to equalize the temperature.
In addition the material acts as a vibration suppressor with respect to acoustic interference.
In this embodiment a thermoelectric element 37, e.g. a peltier element, is located
in the space formed in between the bottom ends of the outer cooling flange 40 and
the inner temperature equalization 39.
[0051] By a suitable choice of construction materials the device can be passively stabilized.
the requirement , in order to have the radiation frequency as stable as possible with
respect to temperature influences, is that the change in optical length of the resonator
of the laser device, that is in the combined optical length of laser element and external
cavity, is minimized.
[0052] The rotationally symmetric construction of the fixed laser in Fig. 1 implies that
the joining together can be carried out in such a way that the inside of the laser
becomes hermetically sealed off from the outer atmosphere. In this way the fixed laser
frequency is not influenced by alternations in air pressure and humidity. The hermetic
sealing also implies that the laser element is protected from influences by the environment,
that can degrade the radiation properties of the element. It is also possible to replace
the ordinary air in the laser cavity by an inert gas.
[0053] The embodiments shown shall only be considered as examples of possible variations
of the fixed laser.
Passive thermal stability
[0054] It is unavoidable that the optical resonator length l
o changes with variations in temperature. Contributions among others come from:
A) Thermal expansion/contraction of the laser element 1, the collimator lens 2 and
the mechanical arrangements 7, 10, 11 and 12, which keep the optical parts in their
places.
B) Changes in the refractive indices of the optical components of the cavity with
temperature, dn/dT.
[0055] Changes (1/n) dn/dT in the laser element 1 can for instance be of the order of 5x10
-5 K
-1 and in the lens 2 of the order of 10
-6 K
-1.
[0056] All these contributions will add with their respective magnitudes and signs. The
ambitions should therefore be to get as small as possible a "vector sum" in adding
the contributions.
[0057] There are in the resonator with the geometrical length l a number of optical elements
in form of optical components and air, which may be numbered with a running index
i.
- l =
- geometrical resonator length = Σ ai
- ai =
- the length of an element
- αi =
- its expansion coefficient
- ni =
- its refractive index
[0058] The optical length of the resonator is

where Σ implies a summation over all elements i. The variation of the optical resonator
lens l
o with temperature is

[0059] Where DER means the derivative with respect to the temperature T.
[0060] In order to get as small as possible a wavelength change in the radiation when the
temperature changes, the design of the resonator should be chosen such as to minimize
DER l
o according to (3).
[0061] A further thermal effect is that the grating changes its spatial groove frequency
with temperature. It is therefore advantageous to choose a substrate material with
as small a thermal expansion coefficient as possible. Another alternative would be
to mount the grating in such a way, that it turns with a temperature change and thereby
satisfies the grating equation (1) for a constant wavelength output.
Alternation and control of the frequency of the fixed laser
[0062] In adjusting the fixed laser to lasing, by turning an optical component, e.g. the
laser element 1, the lens 2 or the grating 3, in such a way that the line LO becomes
perpendicular to the grating groove direction G, the wavelength at which the laser
emits is not completely predictable. One can only predict that it will lie within
a certain wavelength interval, that is determined by the inaccuracy in mechanical
manufacturing and mounting of the laser. The laser, with a turning arrangement for
adjustment of one component, becomes a fixed frequency laser with a not altogether
predetermined wavelength. The laser can be used for a number of applications that
have been touched upon above.
[0063] If one wants to be able to adjust the laser to a given frequency, a second adjustment
arrangement has to be introduced. With such an arrangement that turns one of the optical
components about a fixed axis, one can change the angle α between the normal N to
the grating surface and the direction LO of the collimated radiation 5 in Fig. 5,
maintaining the angle Φ = 90°. Such a rotation can be realized by turning the grating
about a fixed axis parallel to the direction G of the grating grooves. As a consequence
of the initial inaccuracy in lining up the optical elements in the device, the rotational
axis of the grating and the grating grooves do not become altogether parallel, they
form an angle of perhaps some milliradians. There is a weak coupling between the adjustment
of α and the maintaining of Φ = 90°. It is estimated that one can alter α with ± 1°
without changing Φ so much, a few tenths of a milliradian, as to alter the lasing
capability of the laser. For a fixed laser, at the wavelength 1,55 µm, this according
to the grating equation (1), corresponds to the wavelength interval 1,55 ± 0,02 pm.
[0064] In the fixed laser it may be more practical to turn some other component that the
grating 3. In the fixed laser 9 of Fig. 5, Φ is adjusted to 90° by turning the tube
11 with the eccentrically fixed laser element 1.
[0065] Fig. 7 shows a base plate of a laser holder 27, fixed by a first weld to the end
surface of the rotatable tube 23. By turning the tube, with the eccentrically placed
laser element 1 one gets a first adjustment arrangement. A second one is obtained
through the fact that the holder constitutes an elastic hinge for turning the laser
element 1 about the axis R.
[0066] The rotational axis of the tube 23 is A. A small turn of the tube displaces the element
1 a distance Δy. The change Δy corresponds to an adjustment of the angle Φ. If a force
F is applied in the upper portion of the hinge perpendicularly to the axis R, the
laser element rotates about the axis R and the laser element is moved a distance Δx,
that is almost perpendicular to Δy. The change Δx corresponds to a change of the angle
α, that is of the wavelength or frequency of the radiation. After the final adjustment
of Δx, the base plate is fixed through the welds 29.
[0067] A trim of the wavelength or frequency can be made in the fixed laser even after the
components have been fixed, and the laser sealed, if the position or attitude of one
of the optical components can be changed by forces from piezoelectric elements or
the like.
[0068] Mode hop free turning can be made if the applied forces turn the grating about an
axis in the manner described in patent application SE 8902948-2 (EP-A-0 491 777).
[0069] A fast frequency modulation of the radiation can for instance be made through modulation
of the length of the cavity, by the action of forces from one or several piezoelectric
elements on some component, e.g. the grating.
[0070] The laser frequency in the sealed fixed laser can also be changed by controlling
the inner temperature of the laser, e.f. the arrangement 37 for temperature control
in Fig. 9. If the laser is operated at a temperature, that is above room temperature,
then the thermoelectric arrangement 37 can be substituted simply by a resistive heater.
This is a much cheaper solution.
Constant and controllable wavelength of the fixed laser
[0071] It is desirable in many cases, e.g. in interferometric measurements, that the laser
radiation maintains a constant wavelength in an outer atmosphere, i.e. that the wavelength
is not influenced by changes in air pressure, temperature and humidity. The parameters
mentioned influence the refractive index of the air, and thereby the wavelength of
the laser radiation.
[0072] In order to maintain the wavelength constant, when the refractive index of the air
varies, a change of the frequency of the fixed laser is required. The frequency can
be controlled by the signal from a wavelength stable interferometer. The error signal
when the wavelength deviates from its fixed value controls the frequency of the fixed
laser. This feed back works to maintain the signal at its fixed value. The corresponding
method can also be used when the outer environment is another gas instead of air.
[0073] The interferometer 45 in Fig. 10, intended for wavelength stabilization, is fixedly
joined to the fixed laser 9. The length of one of the interferometer arms, that ends
with the prism 48, can be controlled by the cylindrical piezoelement 52. Radiation
from the two interferometer arms is brought together on the two detector element 53,
which have the outlets 54. The position of the retroprism 48, and thereby the signals
from the detector elements 53, is modulated via the piezocontrol signal applied at
55. The interferometer must be in atmospheric connection with the space in which the
measurements are made, so that the atmosphere in the interferometer is representative
of the measurement environment.
[0074] The relation between the radiation wavelength in air λ
1, the frequency and the refractive index n
1 is

where the constant c is the speed of light. In order that the wavelength λ
1 remains fixed, the frequency of the fixed laser 9 in Fig. 11 must be changed in such
a way that

[0075] The change in refractive index of the air or of a gas can thus be recorded by the
change in frequency. The frequency change can be measured by joining the laser radiation
15 from the arrangement in Fig. 10 with the radiation from a second fixed laser with
detector as shown in fig. 11, that is sufficiently fast to record the frequency difference
between the first and second laser. The second laser in this case serves as an optical
local oscillator.
Mounting of grating on a grating seat
[0076] The seat 13 onto which the optical grating is to be applied, can be made of e.g.
quartz, ceramics, or metal. The taps can be manufactured with great precision.
[0077] In the two fixed lasers embodiments fig. 4 and fig. 6 respectively the tap of the
seat which supports the grating can be obliquely or perpendicularly cut and ground.
In the oblique case the end surface of the tap typically can form an angle in the
magnitude of 45° with the axis of the tap. In order to produce seats with gratings
to low price many gratings have to be applied at the same time to the seats.
[0078] A method to carry out is the following, fig. 12a. A greater number of grating seats,
e. g. 100 - 400 per dm
2 are placed in parallel bores with good cylindric fitting in a fixture block 70 of
e.g. invar. The seats are fixed, with e.g. an upper clamping device 71 and face grinded
and polished common so that the surface of the tap ends are situated in a plane 72.
A holographic grating is applied by known technique over the common end plane. The
seats with grating applied are cut free from the common holographic layer. The holes
of the seats in the fixture block can have their axes perpendicular to the layer plane
or form an angle with this depending on the oblique cutting of the taps. An alterative
method, fig 12b, to mount grating on the seat end surfaces, by means of a similar
fixture block 70 as above, is to first apply plane ground bases 73, of e.g. quartz,
on the plane ground ends of the taps 7 of the grating seats. The bases can also alternatively
be of piezo electric material which gives possibility to control the length of the
external cavity or to control the distance between the grooves of the grating.
[0079] The substrate are placed in a lateral fixture 74, the thickness of which is somewhat
less than the height of the base. Joining means is applied between the bases and the
taps of the seats and fixation is carried out by heating in oven or drying. During
the fixation the bases are pressed against the taps of the seats by a lower clamping
device 76 with a plane ground upper surface 77, whereby the bases after the fixation
will obtain a common end plane 75 which is defined by the surface.
Production of laser mounting
[0080] The laser mounting in fig. 13a and b; and 14 a and b is designed for simultaneous
production of many mounts by a sheet technique, where the number of mounts can be
of the magnitude of 100 per dm
2. In the production method the base plate 27 should be joined with the ceramics block
82 and the soldering tongue 81. After the joining the separate laser mountings are
cut loose from each other. The laser element 1 then can be soldered to the edge of
the base plate facing upwards and bonding 80 is performed between the element and
the edge of the soldering tongue. The manufacture of the laser mounts certainly may
vary with respect to its details but the main features are the following.
1. A sheet of connected base plates for the laser mount 27 are produced from a metal
disc, e.g. lmm thickness by etching or similar technique.
2. Fastening means e.g. soldering tin, is applied by screen printing, at the points
on the sheet of base plates 84 where the ceramic blocks are to be fixed. Alternatively
mounting surfaces for the ceramic blocks can be obtained by spot dosing of glue.
3. The blocks are placed out on a supporting disc in correct pattern for the joining
to the base plates by use of a lateral fixture
4. The sheet of base plates is positioned above the disc with blocks. By heating or
drying the blocks are fixed to the base plates.
5. A sheet of continuous soldering tongues 81 are manufactured from a metal disc with
a thickness of e.g. 0,3 mm by etching or similar technique.
6. Solder for soldering the tongues to the blocks is applied to the solder tongue
sheet by screen printing. Alternatively spot dosing can be made for adhesive fixing.
7. The sheet with soldering tongues is placed above the ceramic blocks and the tongues
are fixed to the blocks by heating or drying.
8. A bending and exposing tool is applied over the sheet with soldering tongues, whereby
the edge 85 on these is bent over the block edge and the tongues are released from
the common sheet.
9. The continuous base plates are cut loose from each other by means of an exposing
tool, whereafter the separate mountings are ready for mounting of laser elements and
bonding between the element and the bent solder tongue edge.
LIST OF REFERENCE SYMBOLS USED IN THE DRAWINGS OF THE FIGURES
[0081]
- L =
- that portion on the surface of the laser element that emits radiation
- O =
- optical center of the lens 2
- LO =
- line through L and O
- N =
- line normal to the plane of grooves of the grating 3
- G =
- line in the direction of the grating grooves 4
- Φ =
- angle between LO and G
- α =
- angle between LO and N
- K =
- axis of rotation for an optical component
- A =
- main axis of the lining up bore in 10 or 19
- F =
- pressure force
- R =
- hinge axis for turning of 1
- X =
- movement of 1 in the x-direction when turning about R
- Y =
- movement of 1 in the y-direction when turning about A
- 1 =
- laser element
- 2 =
- collimator lens for the inner radiation 5
- 3 =
- reflection grating
- 4 =
- grating groove
- 5 =
- collimated radiation inside the fixed laser
- 6 =
- tube holder for collimator lens 14
- 7 =
- tap on grating seat or seat tap
- 9 =
- fixed laser
- 10 =
- rotationally symmetric main body with lining up bore and turned recesses for attachment
of components
- 11 =
- tube with holder for 1
- 12 =
- tube holder for 2
- 13 =
- grating seat
- 14 =
- collimator lens for the outer radiation 15
- 15 =
- collimated radiation leaving the laser
- 16 =
- head of grating seat
- 17 =
- lining up bore
- 18 =
- fixed laser
- 19 =
- body with lining up bore and turned holds for the components
- 23 =
- tube for holding the laser element
- 27 =
- base plate of laser holder shaped as an elastic hinge
- 28 =
- first laser weld
- 29 =
- laser weld for fixing after turning about R
- 31 =
- welding seam
- 32 =
- welding seam
- 33 =
- welding seam
- 34 =
- welding seam
- 35 =
- fixed laser with temperature control and thermal insulation
- 37 =
- thermoelectric element
- 38 =
- thermal insulation e g silicone rubber, polyurethane or polystyrene
- 39 =
- inner tube for levelling of temperature
- 40 =
- outer cooling flange
- 44 =
- fixed laser with interferometer
- 45 =
- interferometer
- 46 =
- mirror
- 47 =
- retroprism in a first interferometer arm
- 48 =
- retroprism in a second interferometer arm
- 49 =
- reflection prism
- 50 =
- beam split cube
- 52 =
- piezoelectric cylinder
- 53 =
- photodetector
- 54 =
- detector output
- 55 =
- input for voltage to piezoelectric element
- 56 =
- beam split cube
- 61 =
- mirror
- 62 =
- beam split cube
- 63 =
- detector output
- 64 =
- detector
- 65 =
- fixed laser arrangement for measuring of change of refractive index in an outer environment
- 66 =
- fixed laser used as a local oscillator
- 70 =
- fixture block
- 71 =
- upper clamp yoke
- 72 =
- end surface
- 73 =
- plane ground base
- 74 =
- lateral fixture
- 75 =
- end surface
- 76 =
- lower clamp yoke
- 77 =
- upper plane surface
- 80 =
- bonding wire
- 81 =
- solder tongue
- 82 =
- insulating ceramic block
- 84 =
- part of base plate sheet
- 85 =
- edge on soldering tongue
1. Method to arrange and adjust a laser device that is stable with respect to external
and internal environmental influences by setting said device in a lasing condition
to emit at a wavelength λ
0, where deviation between a predefined wavelength and the sole wavelength λ
0, at which the device is capable of lasing is being dependent on the mechanical precision
with which the device can be manufactured and lined up, which laser device comprises
optical components including a laser element (1), which can generate optical radiation
within a wavelength band λ
1- λ
2 containing λ
0, a plain reflection grating (3) with parallel grating grooves, arranged such that
the latter together with a flat reflection surface, which can be the end surface of
the laser element by which the radiation (15) is outputted, forms a resonator, which
selects the radiation wavelength emitted by the laser device, and an optical collimator
(2) which is disposed between the laser element (1) and the grating (3) in order to
collimate radiation emitted from said laser element (1),
characterised in,
that the method further comprises the steps of :
determining an axis K that admits an angle Φ between two directions to vary within
an interval that contains Φ = 90°, whereby said directions consist of a first direction
LO of collimation of the radiation collimated by said optical collimator (2) and a
second direction G parallel to the grating groves;
mounting at least one of said optical components (1, 2, 3) in a holder (11, 12, 13)
to provide a relative movement of said two directions, when said holder is turned
about said axis K to adjust the laser to a lasing condition.
2. Method according to claim 1,
characterised therein,
that for adjusting the wavelength at least one of said optical components (1, 2, 3)
can be turned about an axis R, the axis having a direction such that in turning the
optical component or components the direction G parallel to the grating grooves remains
perpendicular or close to perpendicular to the direction LO of collimation and an
angle of incidence α of the collimated laser radiation to the plane of the grating
grooves is being altered, changing the radiation wavelength within the band λ1- λ2, in which lasing can be maintained.
3. Method according to claim 2,
characterised therein,
that at least one of the optical components (1, 2, 3) can be turned about said axis
R for adjusting the wavelength, by applying a displacement force, e.g. by means of
one or several piezoelectric elements, in such a way that the direction LO of collimation
remains at right angle to the direction G parallel to the grating grooves and,
the angle of incidence α of the collimated laser radiation to the plane of the grating
grooves is controllable and consequently the wavelength of the radiation.
4. A laser device comprising a main body (10; 19) having a central lining up bore (17)
extending therethrough;
which laser device comprises optical components including a laser element (1), which
can generate optical radiation within a wavelength band λ
1- λ
2, an optical collimator (2), a plain reflection grating (3) with parallel grating
grooves, arranged such that the latter together with a flat reflection surface, which
can be the end surface of the laser element by which the radiation (15) is outputted,
forms a resonator, which selects the radiation wavelength emitted by the laser device,
and which optical collimator (2) is disposed between the laser element (1) and the
grating (3) in order to collimate radiation emitted from said laser element (1),
characterised in,
that the laser device further includes a first tube (12), arranged with the optical
collimator (2), a second tube (11), which holds the laser element (1),
that the first tube (12) is rotatably inserted in the second tube (11) which is rotatably
inserted into the central bore (17) along a main axis A of the main body (10; 19),
that the grating (3) is arranged on a grating seat (13) and rotatably inserted in
a bore of the main body (10; 19), and that the main body is rotatably fitted to a
third tube (6), having an opening arranged with a collimator lens for the laser beam
(15) outputted by the laser device (1), and
that at least one of said optical components is mounted eccentrically with respect
to the main axis A of the central bore of the main body.
5. A laser device according to claim 4,
characterised therein,
that the grating is mounted on an obliquely chamfered cylindrical tap (7) of the grating
seat (13) and that the tap is inserted into the central lining-up bore (17).
6. A laser device according to claim 4,
characterised therein,
that the grating is placed on an obliquely or perpendicularly cut cylindrical tap
(7) of the grating seat (13) and that the tap (7) is inserted into a bore in the main
body (19), the axis of said tap being in a direction that is different from that of
said main axis A.
7. A laser device according to claims 4-6,
characterised therein,
that the laser element (1) is fixed eccentrically with respect to said axis A on a
carrier (27), part of which constitutes an elastic hinge, arranged to displace the
laser element (1), and that the hinge after adjustment is fixable.
8. A laser device according to claims 7,
characterised therein,
that the hinge is fixed by means of welding (29).
9. A laser device according to any of the claims 4-8,
characterised therein,
that the position of the flat reflection surface relative to the grating is arranged
variable to alter the radiation frequency, while maintaining an angle Φ formed between
the direction LO of the collimation of the radiation collimated by the collimator
(2), which is disposed between the laser element and the grating and the direction
G along the grating grooves, at 90°.
10. A laser device according to claim 9,
characterised therein,
that one or more piezoelectric elements (52) are arranged to provide the variation.
11. A laser device according to any of claims 4-10,
characterised therein,
that the device includes materials having different thermal expansion coefficients.
12. A laser device according to any of the claims 4-11,
characterised therein,
that said device includes means to keep the temperature constant in the laser device
through supply or removal of heat, thereby stabilising the optical frequency.
13. A laser device according to any of the claims 4-12,
characterised therein,
that the laser device is hermetically sealed through welding, soldering or cementing,
such that the refractive index in the inner environment is not influenced by changes
in pressure, humidity and gas composition in the outer environment.
14. A laser device according to any of the claims 4-13,
characterised therein,
that a wavelength measuring interferometer (45) is arranged to transmit a signal to
control the frequency in the laser device, which measuring interferometer (45) is
located outside the main body (10; 19), such that the wavelength of the radiation
emitted from the laser element is stabilised in an outer environment with varying
refractive index.
15. A laser device according to claim 14,
characterised therein,
that the interferometer (45) mentioned above is fixedly joined to the laser (9).
16. A laser device according to claim 14 or 15,
characterised therein,
that another laser device (66) which acts as a local oscillator with a constant laser
light frequency is arranged, whereby the wavelength of the laser light of the laser
device (9) controlled by the wavelength measuring interferometer (45) is kept constant
in an outer environment with varying refractive index while the laser light frequency
in the laser device (9) itself varies accordingly, and
that means (53, 64) are arranged to measure variation in frequency differences between
the laser device (9) controlled by the interferometer and the another laser device
(66) to determine a change in refractive index in the outer environment from the relation
ν x n = constant, where ν is optical light frequency and n is the refractive index.
17. Method to fabricate laser devices according to any of claims 4-16,
characterised in that the method comprises the steps of forming the gratings on
seats (13) having taps (7) which are placed in a common fixture block (70) with parallel
cylindrical bores fitted to each seat tap (7), whereby the seats are face grinded
and polished so that on one side of the fixture block (70) the end surfaces of the
tap ends are situated in a common plane (72),
forming a holographic grating on the tap ends which are situated in the common plane
(72), and rotatably inserting the taps (7) with the gratings formed on the seats (13)
into the bores of the main bodies.
18. Method to fabricate laser devices according to any of claims 4-16,
characterised in that the method comprises the step of
mounting said gratings on seat end surfaces of seat taps (7) by means of a fixture
block (70), by first applying plane ground bases (73) on plane ground ends of said
taps (7) of the grating seats (13), then applying said gratings to said ground bases
(73), and rotatably inserting the taps (7) with the gratings into the bores of the
main bodies.
19. A method according to claim 18,
characterised therein,
that the bases (73) are made of piezoelectric material or quartz.
1. Verfahren zum Anordnen und Justieren einer Laservorrichtung, indem die Vorrichtung
in einen Zustand versetzt wird, in dem Laserstrahlen mit einer Wellenlänge λ
o ausgestrahlt werden, wobei eine Abweichung zwischen einer vorbestimmten Wellenlänge
und der alleinigen Wellenlänge λ
o, mit der die Vorrichtung Laserstrahlen aussenden kann, von der mechanischen Genauigkeit
abhängt, mit der die Vorrichtung hergestellt und aufgestellt werden kann, und wobei
die Laservorrichtung optische Komponenten einschließlich eines Laserelements (1),
das die optische Strahlung innerhalb eines Wellenlängenbandes λ
1 - λ
2, das die Wellenlänge λ
o enthält, erzeugen kann, eines ebenen Reflektionsgitters (3) mit parallelen Gittereinschnitten,
die so angeordnet sind, daß die parallelen Gittereinschnitte zusammen mit einer flachen
Reflektionsoberfläche, die das Ende der Oberfläche des Laserelements darstellen kann,
durch die die Strahlung (15) austritt, einen Resonator bilden, der die Wellenlänge
der Strahlung auswählt, die durch die Laservorrichtung ausgestrahlt wird, und eines
optischen Kollimators (2) aufweist, der zwischen dem Laserelement (1) und dem Gitter
(3) angeordnet ist, um die Strahlung, die von dem Laserelement (1) ausgesendet wird,
einzustellen,
dadurch gekennzeichnet, daß
das Verfahren weiterhin folgende Schritte aufweist:
Bestimmung einer Achse K, die einen Winkel Φ zwischen zwei Richtungen zugesteht, um
innerhalb eines Intervalls, das Φ = 90° beinhaltet, zu variieren, wobei die Richtungen
eine erste Richtung LO der Kollimation der Strahlung, die von dem optischen Kollimator
(2) kollimiert bzw. eingestellt wird, und eine zweite Richtung G parallel zu den Gittereinschnitten
umfaßt; und
Einbau zumindest einer optischen Komponente (1, 2, 3) in einer Halterung (11, 12,
13), um für eine relative Bewegung in beiden Richtungen zu sorgen, wenn die Halterung
um die Achse K gedreht wird, um den Laser so zu justieren, daß Laserstrahlen ausgesendet
werden.
2. Verfahren gemäß Anspruch 1, dadurch gekennzeichnet, daß zumindest eine der optischen
Komponenten (1, 2, 3) zur Justierung der Wellenlänge um eine Achse R gedreht werden
kann, die eine solche Richtung aufweist, daß durch Drehung der optischen Komponente
oder Komponenten die Richtung G parallel zu den Gittereinschnitten, senkrecht oder
nahezu senkrecht zur Richtung LO der Kollimation bleibt, und ein Einfallswinkel α
der kollimierten bzw. eingestellten Laserstrahlung auf die Ebene der Gittereinschnitte
geändert wird, wobei sich die Wellenlänge der Strahlung innerhalb des Bandes λ1 - λ2 ändert, indem ein Lasern aufrecht erhalten werden kann.
3. Verfahren gemäß Anspruch 2, dadurch gekennzeichnet, daß
zumindest eine der optischen Komponenten (1, 2, 3) um die Achse R zur Einstellung
der Wellenlänge gedreht werden kann, wobei eine Versetzungskraft angewendet wird,
zum Beispiel mittels eines oder mehrerer piezoelektrischer Elemente, in der Art, daß
die Richtung LO der Kollimation im rechten Winkel zur Richtung G, parallel zu den
Gittereinschnitten, bleibt, und
der Einfallswinkel α der eingestellten Laserstrahlung zur Ebene der Gittereinschnitte
und folglich die Wellenlänge der Strahlung steuerbar ist.
4. Laservorrichtung mit einem Hauptkörper (10; 19), der eine sich dazwischen hindurch
erstreckende zentrale Ausrichtungsbohrung 17, wobei die Laservorrichtung optische
Komponenten aufweist, einschließlich eines Laserelements (1), welches optische Strahlung
innerhalb eines Wellenlängenbandes λ1 - λ2 erzeugen kann, eines optischen Kollimators (2), und eines ebenen Reflektionsgitters
(3) mit parallelen Gittereinschnitten aufweist, die so angeordnet sind, daß die letzteren
zusammen mit einer flachen Reflektionsoberfläche, die die Endoberfläche des Laserelements
sein kann, von dem die Strahlung (15) ausgesendet wird, einen Resonator bilden, der
die Strahlungswellenlänge auswählt, welche von der Laservorrichtung ausgesendet wird,
wobei der optische Kollimator (2) zwischen dem Laserelement (1) und dem Gitter (3)
angeordnet ist, um die Strahlung einzustellen, die vom Laserelement (1) ausgestrahlt
wird,
dadurch gekennzeichnet, daß
die Laservorrichtung weiterhin ein erstes Rohr (12), das am optischen Kollimator (2)
angeordnet ist, und ein zweites Rohr (11) aufweist, welches das Laserelement (1) hält,
wobei das erste Rohr (12) in das zweite Rohr (11) drehbar eingesetzt ist, welches
in die zentrale Bohrung entlang einer Hauptachse A des Hauptkörpers (10; 19) drehbar
eingesetzt ist, wobei das Gitter (3) an einem Gittersitz (13) angeordnet und in eine
Bohrung des Hauptkörpers (10; 19) drehbar eingesetzt ist, und der Hauptkörper drehbar
in ein drittes Rohr (6) eingepaßt ist, welches eine Öffnung mit einer angeordneten
Kollimatorlinse von der Laservorrichtung (1) ausgesendeten Laserstrahl (15) aufweist,
und wobei wenigstens eine der optischen Komponenten exzentrisch in Bezug auf die Hauptachse
A der Zentrahlbohrung des Hauptkörpers montiert ist.
5. Laservorrichtung gemäß Anspruch 4, dadurch gekennzeichnet, daß das Gitter an einem
schräg abgekanteten zylindrischen Verschlußstopfen bzw. Stopfen (7) des Gittersitzes
(13) montiert ist, und daß der Stopfen in die zentrale Ausrichtungsbohrung (17) eingesetzt
wird.
6. Laservorrichtung gemäß Anspruch 4, dadurch gekennzeichnet, daß das Gitter auf einem
schräg oder senkrecht geschnittenen zylindrischen Stopfen (7) des Gittersitzes (13)
angeordnet ist, und daß der Stopfen (7) in eine Bohrung des Hauptkörpers (19) eingesetzt
wird, wobei die Achse des Stopfens in einer Richtung verläuft, die sich von der Hauptachse
A unterscheidet.
7. Laservorrichtung gemäß den Ansprüchen 4 bis 6, dadurch gekennzeichnet, daß das Laserelement
(1) exzentrisch in Bezug auf die Achse A auf einem Träger (27) angebracht ist, wobei
ein Teil von diesem ein elastisches Scharnier aufweist, das zur Verschiebung des Laserelements
(1) angeordnet ist, und wobei das Scharnier nach der Justierung fixierbar ist.
8. Laservorrichtung gemäß Anspruch 7, dadurch gekennzeichnet, daß das Scharnier mittels
Schweißung (29) fixiert ist.
9. Laservorrichtung gemäß einem der Ansprüche 4 bis 8, dadurch gekennzeichnet, daß die
Position der flachen Reflektionsoberfläche relativ zum Gitter veränderbar angeordnet
ist, um die Strahlungsfrequenz zu ändern, während ein Winkel Φ, der zwischen der Kollimationsrichtung
LO der Strahlung, die von dem zwischen dem Laserelement und dem Gitter angeordneten
Kollimator (2) eingestellt wird, und der Richtung G entlang der Gittereinschnitte
gebildet wird, zu 90° beibehalten wird.
10. Laservorrichtung gemäß Anspruch 9, dadurch gekennzeichnet, daß für vorgesehene Veränderbarkeiten
ein oder mehrere piezoelektrische Elemente (52) angebracht sind.
11. Laservorrichtung gemäß einem der Ansprüche 4 bis 10, dadurch gekennzeichnet, daß die
Vorrichtung Materialien aufweist, die verschiedene thermische Expansionskoeffizienten
haben.
12. Laservorrichtung gemäß einem der Ansprüche 4 bis 11, dadurch gekennzeichnet, daß die
Vorrichtung Mittel aufweist, um die Temperatur in der Laservorrichtung durch eine
Zufuhr oder eine Abfuhr von Hitze konstant zu halten, wodurch die optische Frequenz
stabilisiert wird.
13. Laservorrichtung gemäß einem der Ansprüche 4 bis 12, dadurch gekennzeichnet, daß die
Laservorrichtung durch Schweißung, Löten oder Zementation hermetisch abgedichtet ist,
so daß der Brechungsindex in der inneren Umgebung nicht durch Änderungen des Drucks,
der Luftfeuchtigkeit und der Gaszusammensetzung der äußeren Umgebung beeinflußt wird.
14. Laservorrichtung gemäß einem der Ansprüche 4 bis 13, dadurch gekennzeichnet, daß ein
Wellenlängen-Meßinterferometer (45) angebracht ist, um ein Signal zum Steuern der
Frequenz der Laservorrichtung zu übermitteln, wobei das Meßinterferometer (45) außerhalb
des Hauptkörpers (10; 19) angeordnet ist, so daß die Wellenlänge der Strahlung, die
vom Laserelement ausgestrahlt wird, in einer äußeren Umgebung mit variierendem Brechungsindex
stabilisiert wird.
15. Laservorrichtung gemäß Anspruch 14, dadurch gekennzeichnet, daß das Interferometer
(45) fest mit dem Laser (9) verbunden ist.
16. Laservorrichtung gemäß Anspruch 14 oder 15, dadurch gekennzeichnet, daß
eine weitere Laservorrichtung (66), die als lokaler Oszillator arbeitet, mit einer
konstanten Laserlichtfrequenz angebracht ist, wobei die Wellenlänge des Laserlichts
der von dem Wellenlängen-Meßinterferometer (45) gesteuerten Laservorrichtung 9 in
einer äußeren Umgebung mit unterschiedlichen Brechungsindexen konstant gehalten wird,
während die Frequenz des Laserlichts in der Laservorrichtung 9 selbst entsprechend
variiert, und
Einrichtungen (53, 64) zur Messung von Veränderungen der Frequenzunterschiede zwischen
der von dem Interferometer gesteuerten Laservorrichtung (9) und der weiteren Laservorrichtung
(66) angebracht sind, um eine Änderung des Brechungsindex in der äußeren Umgebung
aus der Beziehung ν x n = konstant zu bestimmen, wobei ν die optische Lichtfrequenz
und n der Brechungsindex bedeuten.
17. Verfahren zur Herstellung von Laservorrichtungen gemäß einem der Ansprüche 4 bis 16,
gekennzeichnet durch folgende Schritte:
Bilden der Gitter auf Sitzen (13) mit die Stopfen (7), welche in einen gemeinsamen
Installationsblock (70) mit parallelen zylindrischen Bohrungen eingesetzt sind, die
an die jeweiligen Sitzstopfen (7) angepaßt sind, wobei die Sitze an der Stirnseite
geschliffen und poliert werden, so daß auf einer Seite des Installationsblocks (70)
die Endoberflächen der Stopfenenden in einer gemeinsamen Ebene (72) zu liegen kommen,
Ausbilden eines holographischen Gitters auf den Stopfenenden, die in einer gemeinsamen
Ebene (72) liegen, und
Drehbarer Einsatz der Stopfen (7) und der an den Sitzen (13) ausgebildeten Gitter
in die Bohrungen der Hauptkörper.
18. Verfahren zur Herstellung von Laservorrichtungen gemäß einem der Ansprüche 4 bis 16,
dadurch gekennzeichnet, daß das Verfahren folgende Schritte aufweist:
Montieren der Gitter der auf Sitz-Endoberflächen der Sitzstopfen (7) mittels eines
Installationsblocks (70), indem als erstes eben geschliffene Basiskörper (73) an den
eben geschliffenen Enden der Basiskörper der Stopfen (7) der Gittersitze (13) angebracht
werden, und dann die Gitter an den Basiskörper (73) angebracht werden, und
Drehbarer Einsatz der Stopfen (7) mit den Gittern in die Bohrungen der Hauptkörper.
19. Verfahren gemäß Anspruch 18, dadurch gekennzeichnet, daß die Basiskörper (73) aus
piezoelektrischem Material oder Quarz bestehen.
1. Méthode pour positionner et ajuster un dispositif à laser qui est stable par rapport
aux influences de l'environnement externe et interne en réglant ledit dispositif dans
des conditions d'amorçage du laser afin d'émettre sur une longueur d'onde λo, l'écart entre une longueur d'onde prédéfinie et la longueur d'onde unique λo à laquelle le dispositif est en mesure de s'amorcer étant fonction de la précision
mécanique avec laquelle le dispositif peut être construit et aligné, ledit dispositif
à laser comprenant des composants optiques dont un élément laser (1) susceptible d'émettre
un rayonnement optique dans une bande de longueur d'onde λ1 - λ2 dans laquelle se situe λo, un réseau de diffraction plan (3) à stries de diffraction parallèles disposé de
telle sorte que ces dernières, associées à une surface de réflexion plane qui peut
être la surface terminale de l'élément laser par laquelle sort le rayonnement (15),
forment un résonateur qui discrimine la longueur d'onde du rayonnement émis par le
dispositif à laser, et un collimateur optique (2) disposé entre l'élément laser (1)
et le réseau de diffraction (3) afin de collimater le rayonnement émis par ledit élément
laser (1), caractérisée en ce que la méthode comprend en outre les étapes de :
détermination d'un axe K qui détermine un angle Φ variable dans un intervalle incluant
la valeur Φ = 90° entre deux directions, lesdites directions étant constituées par
une première direction LO de collimation du rayonnement collimaté par ledit collimateur
optique (2) et une seconde direction G parallèle aux stries de diffraction ; montage
de l'un au moins desdits composants optiques (1, 2, 3) sur un support (11, 12, 13)
pour permettre le déplacement relatif desdites deux directions lorsque ledit support
est tourné autour dudit axe K pour régler le laser en conditions d'amorçage.
2. Méthode selon la revendication 1, caractérisée en ce que, pour l'ajustage de la longueur
d'onde, l'un au moins desdits composants optiques (1, 2, 3) peut être tourné autour
d'un axe R, cet axe étant orienté de telle sorte qu'en tournant le - ou les - composant(s)
optique(s), la direction G parallèle aux stries de diffraction reste normale ou pratiquement
perpendiculaire à la direction de collimation LO, l'angle d'incidence α du rayonnement
laser collimaté par rapport au plan des stries de diffraction étant modifié, ce qui
fait varier la longueur d'onde du rayonnement dans la bande λ1 - λ2 dans laquelle l'amorçage peut être maintenu.
3. Méthode selon la revendication 2, caractérisée en ce que l'un au moins desdits composants
optiques (1, 2, 3) peut être tourné autour dudit axe R pour ajuster la longueur d'onde,
en exerçant une force de déplacement, par exemple au moyen d'un ou plusieurs éléments
piézoélectriques, de telle sorte que la direction de collimation LO forme toujours
un angle droit par rapport à la direction G parallèle aux stries de diffraction, et
en ce que l'angle d'incidence α du rayonnement laser collimaté par rapport au plan
des stries de diffraction est ajustable, et par conséquent la longueur d'onde du rayonnement
également.
4. Dispositif à laser comprenant un corps principal (10 ; 19) doté d'un alésage central
d'alignement (17) qui le traverse ;
ledit dispositif à laser comportant des composants optiques dont un élément laser
(1) susceptible d'émettre un rayonnement optique dans une bande de longueur d'onde
λ1 - λ2, un collimateur optique (2), un réseau de diffraction plan (3) à stries de diffraction
parallèles, disposé de telle sorte que ces dernières, associées à une surface de réflexion
plane qui peut être la surface terminale de l'élément laser par laquelle sort le rayonnement
(15), forment un résonateur qui discrimine la longueur d'onde du rayonnement émis
par le dispositif à laser, ledit collimateur optique (2) étant disposé entre l'élément
laser (1) et le réseau de diffraction (3) afin de collimater le rayonnement émis par
ledit élément laser (1), caractérisée en ce que le dispositif à laser comprend en outre un premier tube (12) positionné avec le collimateur
optique (2) et un second tube (11) supportant l'élément laser (1),
en ce que le premier tube (12) est monté de façon à pouvoir tourner à l'intérieur
du second tube (11) lui-même mobile en rotation dans l'alésage central (17) selon
un axe principal A du corps principal (10 ; 19),
en ce que le réseau de diffraction (3) est positionné dans un logement de diffraction
(13) et mobile en rotation dans un alésage du corps principal (10 ; 19),
en ce que le corps principal est monté en rotation dans un troisième tube (6) ayant
une ouverture comportant une lentille de collimation pour le faisceau laser (15) émis
par le dispositif à laser (1), et
en ce que l'un au moins desdits composants optiques est monté de façon excentrée par
rapport à l'axe principal A de l'alésage central du corps principal.
5. Dispositif à laser selon la revendication 4, caractérisé en ce que le réseau de diffraction
est monté sur un insert cylindrique (7) à chanfrein oblique par rapport au logement
de diffraction (13) et en ce que l'insert est ajusté à l'intérieur de l'alésage d'alignement
central (17).
6. Dispositif à laser selon la revendication 4, caractérisé en ce que le réseau de diffraction
est placé sur un insert cylindrique (7) coupé selon un plan oblique ou perpendiculaire
dans le logement de diffraction (13),
et en ce que l'insert (7) est ajusté à l'intérieur d'un alésage du corps principal
(19), l'axe dudit insert étant orienté dans une direction différente de celle dudit
axe principal A.
7. Dispositif à laser selon l'une quelconque des revendications 4 à 6, caractérisé en
ce que l'élément laser (1) est fixé de façon excentrée par rapport audit axe A sur
un support (27) dont une partie constitue une charnière élastique conçue pour déplacer
l'élément laser (1),
et en ce que la charnière peut être immobilisée après avoir été ajustée.
8. Dispositif à laser selon la revendication 7, caractérisé en ce que la charnière est
immobilisée au moyen d'une soudure (29).
9. Dispositif à laser selon l'une quelconque des revendications 4 à 8, caractérisé en
ce que la position de la surface plane de réflexion par rapport au réseau de diffraction
peut être modifiée pour faire varier la fréquence du rayonnement, tout en maintenant
égal à 90° l'angle Φ que forment entre elles la direction de collimation LO du rayonnement
collimaté par le collimateur (2) disposé entre l'élément laser et le réseau de diffraction
et la direction G parallèle aux stries de diffraction.
10. Dispositif à laser selon la revendication 9, caractérisé en ce qu'un ou plusieurs
éléments piézoélectriques (52) sont prévus pour produire la variation.
11. Dispositif à laser selon l'une quelconque des revendications 4 à 10, caractérisé en
ce que le dispositif comporte des matériaux ayant des coefficients de dilatation thermique
différents.
12. Dispositif à laser selon l'une quelconque des revendications 4 à 11, caractérisé en
ce que ledit dispositif comporte un moyen permettant de maintenir constante la température
à l'intérieur du dispositif à laser, par apport ou évacuation de chaleur, ce qui stabilise
la fréquence optique.
13. Dispositif à laser selon l'une quelconque des revendications 4 à 12, caractérisé en
ce que le dispositif à laser est scellé de façon hermétique par soudage, brasure ou
collage, de telle sorte que l'indice de réfraction de l'environnement intérieur ne
soit pas influencé par des variations de pression de degré hygrométrique ou par la
composition d'un gaz de l'environnement extérieur.
14. Dispositif à laser selon l'une quelconque des revendications 4 à 13, caractérisé en
ce qu'un interféromètre de mesure de longueur d'onde (45) est prévu pour transmettre
un signal de commande de la fréquence du dispositif à laser, ledit interféromètre
de mesure (45) étant placé à l'extérieur du corps principal (10 ; 19) de telle sorte
que la longueur d'onde du rayonnement émis par l'élément laser est rendue stable dans
un environnement extérieur où l'indice de réfraction varie.
15. Dispositif à laser selon la revendication 14, caractérisé en ce que l'interféromètre
(45) susdit est associé de façon fixe au laser (9).
16. Dispositif à laser selon l'une ou l'autre des revendications 14 et 15, caractérisé
en ce qu'il est prévu un second dispositif à laser (66) servant d'oscillateur local
avec une fréquence de rayon laser constante, la longueur d'onde du rayon laser du
dispositif à laser (9) pilotée par l'interféromètre de mesure de longueur d'onde (45)
étant maintenue constante dans un environnement extérieur à indice de réfraction variable,
la fréquence du rayon laser du dispositif à laser (9) lui-même variant en conséquence,
et
en ce que des moyens (53, 64) sont prévus pour mesurer l'écart de fréquence entre
le dispositif à laser (9) piloté par l'interféromètre et le second dispositif à laser
(66), afin de déterminer la variation d'indice de réfraction dans l'environnement
extérieur à partir de la relation ν x n = constante, ν étant la fréquence optique
du rayon et n l'indice de réfraction.
17. Méthode de fabrication de dispositifs à laser selon l'une quelconque des revendications
4 à 16, caractérisée en ce que la méthode comprend les étapes de :
formation de réseaux de diffraction dans des logements (13) comportant des inserts
(7) qui sont placés dans un bloc de montage commun (70) comportant des alésages cylindriques
parallèles ajustés à chaque insert (7), les inserts étant meulés et polis en surface
de telle sorte que, d'un côté du bloc de montage commun (70), les surfaces frontales
des extrémités des inserts soient situées dans un même plan (72),
formation d'un réseau de diffraction holographique sur les extrémités des inserts
qui sont situées dans le plan commun (72), et
mise en place des inserts (7) avec les réseaux de diffraction formés dans les logements
(13) des alésages des corps principaux, de telle sorte qu'ils soient mobiles en rotation.
18. Méthode de fabrication de dispositifs à laser selon l'une quelconque des revendications
4 à 16, caractérisée en ce que la méthode comprend les étapes de :
montage desdits réseaux de diffraction sur les surfaces terminales des inserts (7)
au moyen d'un bloc de montage commun (70), en appliquant tout d'abord des plaques
de base planes (73) sur les extrémités planes desdits inserts (7) des logements de
réseau de diffraction (13), puis en appliquant lesdits réseaux de diffraction sur
lesdites plaques de base planes (73), et
l'insertion des inserts (7) avec leurs réseaux de diffraction dans les alésages des
corps principaux, de telle sorte qu'ils soient mobiles en rotation.
19. Méthode selon la revendication 18, caractérisée en ce que les bases (73) sont faites
en matériau piézoélectrique ou en quartz.